SpaceAtlas Space Object Data
NASA JPL SBDB · 2013 CV83

2013 CV83

2013 CV83 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.433 AU it takes 1.72 yr to circle the Sun.

Apollo Observations: 90
Orbital Period · P
1.72 yr
v(q)
40.5 km/s
v(Q)
15.3 km/s
Diameter · ≈
0.06 km
TJ
4.56
Eccentricity · e
0.4529

Orbit and dynamics

The path is an ellipse reaching 0.784 AU from the Sun at perihelion and 2.082 AU at aphelion, a radial span of 1.298 AU.

Applying Kepler's third law to a = 1.433 AU gives an orbital period of 1.72 yr, or about 627 days.

The high eccentricity (0.453) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 4.56° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 40.5 km/s at perihelion and falls to 15.3 km/s at aphelion.

Because q < 1 AU and Q > 1 AU, this orbit geometrically intersects the region of Earth's orbit.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 23.95 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.06 km.

Observation record and orbit quality

The current orbit solution is based on 90 observations and has a weighted RMS residual of 0.587 arcseconds.

Condition code U = 0 means the orbit is very well determined, leaving only a small uncertainty in the future ephemeris.

About these computed values

Orbital periods, perihelion and aphelion speeds, and diameter estimates on this page are computed by SpaceAtlas from the JPL SBDB orbital elements. They are derived quantities, not values copied from the source catalogue.

Orbital Parameters

Semi-Major Axis
1.433 AU
Eccentricity
0.4529
Perihelion
0.784 AU
Aphelion
2.082006 AU
Inclination
4.56°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
303.62°

Orbit diagram

The Sun sits at the focus (orange). Earth's orbit is the grey circle at 1 AU. The red dot marks the object's position at the catalog epoch.

3D orbit (interactive)

Drag to rotate; scroll or pinch to zoom. The Sun is at the focus (orange), Earth's orbit is the grey ring at 1 AU, and the red dot marks the object's current position.

Close approaches

Predicted close approaches to Earth, from NASA's Center for Near-Earth Object Studies (CNEOS).

Date (UTC)Miss distanceVelocity
2031-Sep-18 17:51 0.032791 AU
4905490 km
11.27 km/s
2037-Feb-21 09:54 0.258589 AU
38684291 km
19.71 km/s
2043-Oct-22 17:00 0.175320 AU
26227427 km
9.10 km/s
2049-Mar-03 01:57 0.452006 AU
67619063 km
25.50 km/s
2055-Aug-30 23:31 0.452843 AU
67744351 km
5.42 km/s
2055-Dec-08 22:21 0.209883 AU
31398120 km
10.22 km/s
2062-Aug-28 11:26 0.322258 AU
48209113 km
21.45 km/s
2068-Jan-31 20:19 0.071893 AU
10755078 km
10.09 km/s
2074-Sep-07 14:45 0.135096 AU
20210058 km
15.95 km/s

Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.

Physical Parameters

Diameter
— km
Albedo
—
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
23.95

Orbit Quality

RMS
0.58704
Condition
0
Orbit ID
—
Data source: NASA JPL Small-Body Database · NASA CNEOS. Orbital periods, perihelion and aphelion speeds, and diameter estimates on this page are computed by SpaceAtlas from the JPL SBDB orbital elements. They are derived quantities, not values copied from the source catalogue.

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